IL269761A - Missile provided with a separable nose cone comprising at least one ejectable shell cooperating with a support element - Google Patents

Missile provided with a separable nose cone comprising at least one ejectable shell cooperating with a support element

Info

Publication number
IL269761A
IL269761A IL26976119A IL26976119A IL269761A IL 269761 A IL269761 A IL 269761A IL 26976119 A IL26976119 A IL 26976119A IL 26976119 A IL26976119 A IL 26976119A IL 269761 A IL269761 A IL 269761A
Authority
IL
Israel
Prior art keywords
support element
nose cone
shell cooperating
missile provided
ejectable
Prior art date
Application number
IL26976119A
Other languages
Hebrew (he)
Other versions
IL269761B1 (en
IL269761B2 (en
Original Assignee
Mbda France
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mbda France filed Critical Mbda France
Publication of IL269761A publication Critical patent/IL269761A/en
Publication of IL269761B1 publication Critical patent/IL269761B1/en
Publication of IL269761B2 publication Critical patent/IL269761B2/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F42B10/42—Streamlined projectiles
    • F42B10/46—Streamlined nose cones; Windshields; Radomes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IL269761A 2017-04-21 2018-02-19 Missile provided with a separable nose cone comprising at least one ejectable shell cooperating with a support element IL269761B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1700448A FR3065521B1 (en) 2017-04-21 2017-04-21 MISSILE PROVIDED WITH A SEPARABLE HEADBOARD COMPRISING AT LEAST ONE EJECTABLE SHELL COOPERATING WITH A SUPPORTING ELEMENT
PCT/FR2018/000032 WO2018193170A1 (en) 2017-04-21 2018-02-19 Missile provided with a separable nose cone comprising at least one ejectable shell cooperating with a support element

Publications (3)

Publication Number Publication Date
IL269761A true IL269761A (en) 2019-11-28
IL269761B1 IL269761B1 (en) 2023-12-01
IL269761B2 IL269761B2 (en) 2024-04-01

Family

ID=59974474

Family Applications (1)

Application Number Title Priority Date Filing Date
IL269761A IL269761B2 (en) 2017-04-21 2018-02-19 Missile provided with a separable nose cone comprising at least one ejectable shell cooperating with a support element

Country Status (8)

Country Link
US (1) US10767968B2 (en)
EP (1) EP3392604B1 (en)
JP (1) JP7032431B2 (en)
ES (1) ES2775445T3 (en)
FR (1) FR3065521B1 (en)
IL (1) IL269761B2 (en)
PL (1) PL3392604T3 (en)
WO (1) WO2018193170A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3960639A4 (en) * 2019-04-26 2023-01-18 Kawasaki Jukogyo Kabushiki Kaisha Nose fairing
US11274907B2 (en) * 2020-04-28 2022-03-15 Raytheon Company Shroud driven deployable flight surfaces and method
JP7446915B2 (en) * 2020-05-25 2024-03-11 三菱重工業株式会社 Rectification structure, flying object and spacecraft
CN114046694A (en) * 2021-11-03 2022-02-15 天津爱思达航天科技有限公司 Composite material shell connecting frame reinforcing structure
CN114777576A (en) * 2022-04-08 2022-07-22 湖北航天技术研究院总体设计所 Radome fairing device and rotary side-throwing method
FI130682B1 (en) * 2022-07-11 2024-01-16 Raimo Hirvinen A rocket stage, a rocket and a gliding part

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3706281A (en) * 1971-04-01 1972-12-19 Nasa Method and system for ejecting fairing sections from a rocket vehicle
JPS5640640Y2 (en) * 1972-03-21 1981-09-22
JPH02267500A (en) * 1989-04-10 1990-11-01 Mitsubishi Electric Corp Heat resistant radome for missile
US5263418A (en) * 1992-01-24 1993-11-23 Olin Corporation Hollow point sabot bullet
JPH06313699A (en) * 1993-04-30 1994-11-08 Mitsubishi Heavy Ind Ltd Radome
US5479861A (en) * 1994-01-03 1996-01-02 Kinchin; Anthony E. Projectile with sabot
JP3223171B2 (en) * 1998-12-24 2001-10-29 宇宙開発事業団 Division structure and division method of rocket fairing
DE10240040A1 (en) * 2002-08-27 2004-03-11 BODENSEEWERK GERäTETECHNIK GMBH Guided missile with detachable protective cap
US7082878B2 (en) * 2003-07-01 2006-08-01 Raytheon Company Missile with multiple nosecones
US7549376B1 (en) * 2005-07-15 2009-06-23 The United States Of America As Represented By The Secretary Of The Army Non-lethal projectile carrier
US8519312B1 (en) * 2010-01-29 2013-08-27 Raytheon Company Missile with shroud that separates in flight
DE102010007064B4 (en) * 2010-02-06 2012-03-29 Diehl Bgt Defence Gmbh & Co. Kg Missile head and method of separating a hood from a missile body
US8069791B1 (en) * 2010-03-31 2011-12-06 The United States Of America As Represented By The Secretary Of The Navy Curvilinear sabot system
US8931738B2 (en) * 2012-02-21 2015-01-13 Raytheon Company Releasable radome cover
US9587922B2 (en) * 2013-04-12 2017-03-07 Raytheon Company Attack capability enhancing ballistic sabot
IL232381B (en) * 2014-04-30 2020-02-27 Israel Aerospace Ind Ltd Cover
FR3022885B1 (en) * 2014-06-25 2016-10-21 Mbda France STRUCTURING WALL OF MISSILE, ESPECIALLY FOR THERMAL PROTECTION COFFEE
FR3022995B1 (en) * 2014-06-25 2017-06-09 Mbda France MISSILE PROVIDED WITH A SEPARABLE PROTECTIVE VEST

Also Published As

Publication number Publication date
US10767968B2 (en) 2020-09-08
JP7032431B2 (en) 2022-03-08
PL3392604T3 (en) 2020-06-15
EP3392604A1 (en) 2018-10-24
US20200049474A1 (en) 2020-02-13
WO2018193170A1 (en) 2018-10-25
EP3392604B1 (en) 2020-01-29
JP2020517881A (en) 2020-06-18
ES2775445T3 (en) 2020-07-27
FR3065521A1 (en) 2018-10-26
FR3065521B1 (en) 2019-06-28
IL269761B1 (en) 2023-12-01
IL269761B2 (en) 2024-04-01

Similar Documents

Publication Publication Date Title
IL269761A (en) Missile provided with a separable nose cone comprising at least one ejectable shell cooperating with a support element
IL249531A0 (en) Missile provided with a separable protective fairing
GB201503980D0 (en) An aircraft comprising a foldable aerodynamic structure and an articulation mechanism for a foldable aerodynamic structure
SI3314884T1 (en) Providing enhanced situational-awareness using magnified picture-in-picture within a wide field-of-view optical image
GB201702852D0 (en) A flight system
IL268933A (en) Aircraft provided with a secondary flight assembly
GB2543351B (en) A parachute
ZA201705085B (en) Aerodynamic projectile
EP2927771C0 (en) Flying drone trajectory synchronization
PL3105532T3 (en) Lead-free partial fragmentation bullet with separation mechanism between the rear of the bullet and bullet ogive
SG11202007859SA (en) Droplet ejector
IL269773A (en) Actuation device for ejecting at least one removable part of a missile, particularly a nose
PT3587798T (en) Aerodynamic structure
IL267071A (en) Balancing assembly comprising balancing rings for a missile and missile provided with such a balancing assembly
IL248769A0 (en) Folding wing for a missile and a missile having at least one folding wing arranged thereon
IL262717B (en) Cone comprising a casing for a toy
EP3558470C0 (en) A line ascender
GB2565007B (en) A turbine ring assembly with cold setting
GB2551632B (en) An aircraft propulsion assembly with a filtered cradle
GB2571187B (en) Aircraft galley
PL3263453T3 (en) A rotor and an aircraft provided with such a rotor
ZA201806820B (en) Parachute device for a divisible shell
GB2578572B (en) A sabot
GB2570773B (en) A flight system
HUE062674T2 (en) A novelty breakable shell